A race for a bearing, which is mountable to a mount, has an annular bearing surface with a center axis defining an axis of rotation for the bearing and mutually perpendicular radial and transverse directions relative thereto. The race also has a radial wall that is adapted for mounting the race to the mount in a manner such that a bearing transfer load is transferred between the mount and the race in the transverse direction and the race bearing surface maintains its substantially annular shape independently of a load applied to the mount causing distortion of the mount when the race is mounted to the mount and the mount is loaded.
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10. A combination comprising:
a race for a bearing comprising an annular bearing surface extending about a bearing axis and a wall extending radially from the annular bearing surface;
a mount for the bearing race comprising a center hub formed on the mount; and
a plurality of slots formed on one of the race wall and the hub and a plurality of cooperating bosses formed on the other of the race wall and the hub, each of the slots and the bosses extending in both the radial and transverse directions relative to the bearing axis, the slots and bosses having a close fit in the transverse direction to allow a transfer of a bearing load between the mount and the bearing race, the slots and bosses having a loose fit in the radial direction such that the race bearing surface maintains its substantially annular shape independently of any load applied to the mount tending to cause elastic distortion of the mount along the bearing axis.
1. A combination comprising:
a race for a bearing comprising an annular bearing surface extending about a bearing axis and a wall extending radially from the annular bearing surface;
a mount for the bearing race comprising a center hub formed on the mount; and
at least one slot being formed on one of the race wall and the hub, and at least one cooperating boss being formed on the other of the race wall and the hub, the slot and the boss extending in both radial and transverse directions relative to the bearing axis, the slot and boss engaging with each other in the transverse direction in a manner to transfer a bearing load between the mount and the bearing race, the slot cooperating with the boss to form a gap therebetween in the radial direction sufficient in dimension to allow relative movement between the slot and the boss in the radial direction as the mount is distortionally loaded and elastically deformed along the bearing axis.
13. A bearing race and a mount combination for rotatably mounting a rotating member about a bearing axis, the rotating member being adapted to rotate about an axis perpendicular to the bearing axis wherein rotation of the rotating member about the perpendicular axis creates a centrifugal force so as to apply a load to the mount tending to elastically distort the mount along the bearing axis, the combination comprising:
the bearing race comprising an annular bearing surface and a wall extending radially from the bearing surface, the wall comprising one of a plurality of slots and a plurality of cooperating bosses, and the mount comprising the other of the plurality of slots and the plurality of cooperating bosses, the slots and bosses extending in both the radial and transverse directions relative to the bearing axis, the slots and bosses engaging with each other in the transverse direction to allow a transfer of a bearing load between the mount and the bearing race, the slots being spaced and apart from the bosses in the radial direction to allow relative movement of the bearing race and the mount in a radial direction relative to the bearing axis as the rotating member is centrifugally loaded and elastically deformed along the bearing the bearing axis.
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This invention was developed pursuant to U.S. Government Contract MDA972-98-9-0009 between The Boeing Company and Defense Advanced Research Projects Agency (DARPA).
(1) Field of the Invention
The present invention pertains to a bearing race for a bearing and a mount or support for the bearing. More specifically, the invention pertains to an improved design for a bearing race which maintains its annular bearing surface when it is mounted to a mount and the mount is subjected to a load which causes distortion of the mount. The manner in which the race is connected to the mount prevents the distortion of the mount from being transferred from the mount to the race when the mount is loaded and distorted.
(2) Description of the Related Art
Roller bearings are known in the art and provide an effective means for controlling rotary motion of one object relative to another. Bearings of this type are effective in controlling rotary motion about an axis of rotation. Typically, the roller bearing comprises an outer race and an inner race with a plurality of rollers positioned between the races in rolling contact with the races. Generally, a cage is used to maintain the rollers in a fixed orientation between the races and in rolling contact with the races. In a typical installation of the roller bearing, one of the races is mounted to a journal of a rotating object, for instance, a spindle, and the other of the races is mounted to a fixed object, such as a housing for the spindle. In this way, the rotary motion of the one object may be transferred to the race such that the race and the rotating object rotate through the action of the rollers in a controlled manner relative to the other of the races and the stationary object.
As the rollers of the bearing and the surfaces upon which they roll are critical to ensuring proper operation of the bearing, it is essential that the bearing surfaces and the rollers have tightly controlled dimensions and shapes, including diameter size, roundness, cylindricity, etc. Additionally, it is critical that there be minimal circular run out between the races. Over time, even small imperfections and deviations in the rollers and the bearing surfaces can cause excessive and accelerated wear of the bearing leading to premature failure of the bearing.
Conventional bearings are well suited for applications where there is rotary motion between a shaft and a stationary object. Typically, the races are fixedly attached to their mounts or supports and the mounts are not subjected to external loads which would cause excessive distortion of the mount or support. In applications where there are excessive forces, typically the size of the bearing is increased to compensate for the force and to provide a more rigid connection. However, in applications where size must be constrained and the mounts are subjected to external loads which cause the mounts to distort, a larger bearing cannot be used and the distortion of the mount transfers directly to the race thereby deforming the bearing surface and causing the bearing to fail prematurely.
In the application giving rise to the invention disclosed herein, the roller bearing is an inboard pitch bearing provided in the rotor hub of a helicopter. In this application, the roller bearing provides a rotational hinge about which the helicopter blade pitch is changed. The rotor hub assembly is subjected to an extreme amount of centrifugal force developed from the rotor blades as they rotate to generate lift for the helicopter, and as the rotor hub retains the blades in place under the centrifugal force in which the blades operate, there is distortion of the blade supporting members, including the mounts and supports for the inboard pitch bearing. Designs which have used a conventional roller bearing in this application have had problems because the high centrifugal forces developed by the rotor blades distort the inboard pitch bearing mounts causing deformation of the inboard pitch bearing race and premature failure of the inboard pitch bearing.
Thus, what is needed is a bearing race which is capable of transferring a bearing transfer load to its mount or receiving the bearing transfer load from its mount while the bearing surface or the race maintains its annular shape independently of an external load applied to the mount which distorts the mount. Such a bearing race and mount would be of relatively simple construction and have relatively few parts so that manufacturing, inventory and installation costs associated with the bearing and the mount could be kept to a minimum. Such a race and mount would be part of a compact and lightweight assembly, thereby meeting the stringent space and weight limitations and other constraints dictated by the application.
The present invention overcomes the disadvantages of the prior art by providing a bearing race which is capable of maintaining its annular bearing surface in an annular shape when it is mounted to a mount and the mount is loaded and distorted. The bearing race and mount are designed to prevent the distortion of the mount from being transferred to the race while at the same time allowing bearing transfer loads to be transferred between the mount and the race. The present invention provides for a compact and lightweight design for the bearing race and the bearing race support or mount, and a relatively simple construction and method of manufacture and assembly.
Among the aspects of the present invention is a combination of a race for a bearing and a mount for the bearing race. The bearing race of the combination comprises an annular bearing surface and a wall extending radially from the bearing surface. The bearing race wall is adapted to engage with the mount for mounting the bearing race to the mount. The combination has engaging components that transfer a bearing transfer load between the mount and the race while allowing relative movement of the bearing race and the mount in a radial direction under a distorting load applied to the mount.
In one aspect of the invention, the radial wall comprises a plurality of slots on the radial wall that extend in both the radial and transverse directions, and the slots are formed to cooperate with a plurality of bosses formed on the mount when the race is mounted to the mount. Preferably, the radial wall slots are formed to have a tight fit with the mount bosses in the transverse direction and a loose fit with the mount bosses in the radial direction.
Among other aspects of the present invention is the provision of a combination comprising a race for a bearing and a mount for the race. The race of the combination comprises an annular bearing surface and a radial wall extending from the annular bearing surface adapted for mounting the race to the mount. The bearing race radial wall and the mount each have complementing portions of engaging components for mounting the race to the mount in a manner such that a bearing transfer load is transferred between the mount and the race while the race bearing surface maintains its substantially annular shape independently of any load applied to the mount tending to cause distortion of the mount.
In another aspect of the present invention, a combination of a bearing race and a mount is provided for rotatably mounting a rotating member. The rotating member is adapted to rotate about an axis perpendicular to the bearing axis, and rotation of the rotating member about the perpendicular axis creates a centrifugal force which causes a load to be applied to the mount tending to distort the mount. The bearing race of the combination comprises an annular bearing surface and a wall extending radially from the bearing surface. The wall is adapted to engage with the mount for mounting the bearing race to the mount. The combination has engaging components that are adapted to transfer a bearing transfer load between the mount and the race. The engaging components allow relative movement of the bearing race and the mount in a radial direction under the centrifugal force load.
The present invention provides for a compact design for a bearing and its mount which is lightweight and capable of maintaining its annular shape when the mount or support is subjected to extreme loading. Further objects and features of the invention are revealed in the following detailed description of the preferred embodiment of the invention and in the drawings which follow.
Corresponding reference numbers indicate corresponding parts throughout the several views of the drawings.
In the arrangement shown in
Referring to
The radial wall 32 is provided with a plurality of slots 34, which are contained within the radial wall. As shown in
Referring to
In the present invention, the mount 22 has an outer rim 50 which is spaced from the center hub 40 a distance sufficient to accommodate the race 20 and the other components of the bearing, i.e., the rotational elements, the outer race, and the outer race mount (not shown). Lugs 51 are attached to the outer rim, and in the application herein, the lugs are used to hold the helicopter rotor blades (not shown) to the hub assembly (not shown). The mount center hub 40 has an outer diameter 52 which is sized to provide clearance with an inner diameter 54 of the race.
The center hub 40 is preferably provided with fastener holes 56 which align with the fastener holes 36 on the race. Accordingly, for the present invention, the mount bosses 44 and the mount fastener holes 56 have an alternating pattern on the circular end surface 42 which complements the alternating pattern of the slots 34 and the race fastener holes 36 on the race radial wall 32. Around each of the mount fastener holes 56 is a raised surface or boss 58 which extends axially outward from the circular end surface 42. The mount fastener hole boss 58 is arranged on the circular end surface in a manner to minimize the amount of distortion that may be transferred from the mount to the race when the mount is loaded. Additionally, the mount fastener hole boss 58 has an axial height which is less than the mount boss 44 thereby allowing the mount bosses to engage the race slots 34 while providing relative positioning for the race radial wall 32 above the hub circular end surface 42. As shown in
On the circular end surface 42 on each side of the mount fastener hole boss 58, a compression spring locator hole 62 is provided (
Referring to
As shown in
As can be seen by the drawings and the above description, the bearing race is able to receive a bearing transfer load transferred from the mount, or vice versa, while allowing relative movement between the race and the mount in the radial direction, thereby preventing or at least substantially reducing the transfer of mount distortion to the race. Together, the clearances between the bosses 44 and the slots 34, between the fasteners 38 and the race fastener holes 36, and between the end surface 42 and the radial wall 32 allow for distortion of the mount without the distortion being transferred to the race. Because the race 20 has a floating connection with the mount 22, transfer of mount distortion to the race is substantially reduced.
Although the present invention shows the bearing race formed with slots and the mount formed with bosses, it should be appreciated that these elements may be reversed or interchanged depending upon the application; and therefore, this alternative is considered to be within the scope of the invention. Additionally, the bosses on the mounts are shown to be rectangular in shape so as to cooperate with the rectangular slots in the race. It should be understood that the bosses and slots may be each formed in a geometric shape which cooperates with the other in a manner to enable the bearing transfer load to be transferred from the mount to the bearing race in the transverse direction while allowing relative movement between the race and the mount in the radial direction.
As various changes could be made in the above constructions and methods without departing from the scope of the invention, it is intended that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense. The invention therefore shall be limited solely by the scope of the claims set forth below.
Alexander, John Vernon, Nyhus, Daniel Alan, Soloski, Richard
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Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Dec 19 2002 | ALEXANDER, JOHN V | Boeing Company, the | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 013617 | /0758 | |
Dec 19 2002 | NYHUS, DANIEL A | Boeing Company, the | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 013617 | /0758 | |
Dec 19 2002 | SOLOSKI, RICHARD | Boeing Company, the | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 013617 | /0758 | |
Dec 20 2002 | The Boeing Company | (assignment on the face of the patent) | / | |||
Oct 02 2003 | ALEXANDER, JOHN V | Boeing Company, the | CORRECTIVE ASSIGNMENT TO CORRECT THE STATE OF INCORPORATION OF ASSIGNEE ON ASSIGNMENT PREVIOUSLY RECORDED AT REEL 013617 FRAME 0758 ON DECEMBER 20, 2002 | 014575 | /0649 | |
Oct 02 2003 | NYHUS, DANIEL A | Boeing Company, the | CORRECTIVE ASSIGNMENT TO CORRECT THE STATE OF INCORPORATION OF ASSIGNEE ON ASSIGNMENT PREVIOUSLY RECORDED AT REEL 013617 FRAME 0758 ON DECEMBER 20, 2002 | 014575 | /0649 | |
Oct 02 2003 | SOLOSKI, RICHARD | Boeing Company, the | CORRECTIVE ASSIGNMENT TO CORRECT THE STATE OF INCORPORATION OF ASSIGNEE ON ASSIGNMENT PREVIOUSLY RECORDED AT REEL 013617 FRAME 0758 ON DECEMBER 20, 2002 | 014575 | /0649 |
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